19840612024259A

Accident · Substantial damage

FAA accident report · Bell 205A-1 · Talkeetna, AK · June 12, 1984

Date
June 12, 1984 · 14:30 local
Place
Talkeetna, AK
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
Rotorcraft external load (Part 133)
Damage
Substantial damage
Aircraft
N58116
NTSB investigation
NTSBANC84LA089
Reported as
Bell 205A1
Reported engine
Lycoming T5313A
Fatal injuries
0
Pilot’s flight hours
9,430 total450 in this make and model400 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

Helicopter experienced intensive vibration. Autorotation was accomplished. 32 inches of rotor blade skin missing.

As the FAA filed it

HELICOPTER EXPERIENCED INTENSIVE VIBRATION. AUTOROTATION WAS ACCOMPLISHED. 32 INCHES OF ROTOR BLADE SKIN MISSING.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.

Other reports on N58116 · 1

Matched to the same aircraft by N-number and date.